机械与电子2017，Vol.35Issue(12)：6-10,5.
积冰对飞机操纵特性影响的建模与仿真
Modeling and Simulation of Icing Effects on Aircraft Handling Characteristics
张义浦 1李静 2张志春1
作者信息
- 1. 空军航空大学军事仿真技术研究所,吉林长春130022
- 2. 空军航空大学飞行器动力系,吉林长春130022
- 折叠
摘要
Abstract
Aiming at the wing icing problem,the icing degree parameter was used to describe the ice effects on aircraft aerodynamic parameter;This parameters was introduced into nonlinear six degrees-of-freedom dynamic model of plane;A time-varying simulation model was established with Simulink,which varying with this parameter;By comparing the simulation result with flight test data,the correctness of this is verified;A pitch angle keeping model of closed loop simulation system is designed;In certain flighticing conditions,the open-loop and closed-loop flight simulation were performed;Through the open loop system simulation,studied the effect of ice accretion on aircraft trim characteristics,the flying state and the pilot response effect were also simulated;Through the closed-loop system simulation,the flight status affected by ice accretion processes and the corresponding response of aircraft control was simulated.The simulation results showed that the ice accretion has adverse effects on trim characteristics,aircraft response and automatic driving performance.It's a threat to flight safety.关键词
飞机积冰/程度参数/操纵特性/俯仰姿态保持/仿真Key words
aircraft icing/degree parameter/handling characteristics/pitch-hold model/simulation分类
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张义浦,李静,张志春..积冰对飞机操纵特性影响的建模与仿真[J].机械与电子,2017,35(12):6-10,5.
